CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > Siemens > STAR-CCM+

Grid Independence of Boundary Layer

Register Blogs Community New Posts Updated Threads Search

Like Tree3Likes
  • 1 Post By Luigi_
  • 2 Post By kyle

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   December 13, 2011, 22:58
Default Grid Independence of Boundary Layer
  #1
New Member
 
Luigi Francisco
Join Date: Jan 2011
Posts: 8
Rep Power: 15
Luigi_ is on a distinguished road
Hello,

My question:
When I increase the mesh resolution in the BL, it has the result of reducing the mesh size of the last BL mesh, in comparison to the first mesh volume size of the core flow. Is this a problem, when there is a large step change between the last prism layer mesh, and first core mesh volume?

Model:
I'm modeling channel flow looking at the boundary layer on one wall that starts from a BL trip (modeled with surface roughness near the beginning of the channel). I am using a Reynolds stress turbulence model. I'm confused in how/the need to do a grid independence study for the boundary layer.

Grid independence methodology:
First I refined my core (outside the BL) as needed until I was happy with grid independence for the bulk flow. For these different runs of different mesh size, my boundary layer mesh was always the same-- y+=~0.85, with 20 prism layers across the BL thickness (as calculated from normal flat plate turbulent BL growth).

Now, any insight into the proper methodology to reach grid independence in the BL? Do I, as state above, just increase the number of cells in the BL, while keeping the first mesh size the same to preserve y+=~1.0?

Alternatively, I could also reduce the size of the first mesh, so now it would be even less than y+=~0.85 and it is more refined all the way across the BL.

Also since there seems to be two variables to change (first mesh size, and prism layer number), any advice to know when the BL mesh is sufficient? Since it isn't like bulk flow where you just refine it until your variables of interest aren't changing.

Any insight would be appreciated. Thanks!
Shubhankar94 likes this.
Luigi_ is offline   Reply With Quote

Old   December 14, 2011, 18:55
Default
  #2
Senior Member
 
Join Date: Mar 2009
Location: Austin, TX
Posts: 160
Rep Power: 18
kyle is on a distinguished road
If I am understanding you right, this is something I have always had an issue with...

The prism layer thickness should not be set as a percentage of the base size. This should not even be an option, much less the default behavior.

What you need to do is switch the prism layer thickness size type from "Relative to Base" to "Absolute". Then you can input an actual dimension for your prism layer, and when you change the base size for a mesh independence study it will not effect your y+ values.
sail and Shubhankar94 like this.
kyle is offline   Reply With Quote

Old   December 14, 2011, 19:50
Default
  #3
New Member
 
Luigi Francisco
Join Date: Jan 2011
Posts: 8
Rep Power: 15
Luigi_ is on a distinguished road
Actually, I already have the prism layer thickness as absolute. But if I refine my mesh in the BL, by adding more prism layers, while keeping the thickness of the first cell near the wall constant, and the overall prism layer thickness constant, then my most internal prism layer mesh decreases in size. So now there is a larger discontinuity in mesh size between the innermost prism layer mesh, and the first mesh in the core flow. Is this a problem if there is this big step change in size going from prism layer mesh volume to core mesh volume?

And ultimately, I'm trying to figure out how to make sure my boundary layer mesh is grid independent. Thanks for the reply and looking.
Luigi_ is offline   Reply With Quote

Old   December 14, 2011, 20:01
Default
  #4
Senior Member
 
Join Date: Mar 2009
Location: Austin, TX
Posts: 160
Rep Power: 18
kyle is on a distinguished road
I see what you are saying. This is what Star-CCM+ refers to as "Volume Change." It should be pretty robust over quite a large range. There is a field function for it. The manual suggests anything over 1e-5 is OK, but you may be able to handle even more with the high aspect ratio cells that you have in the prism layer.
kyle is offline   Reply With Quote

Old   December 15, 2011, 03:04
Default
  #5
New Member
 
Luigi Francisco
Join Date: Jan 2011
Posts: 8
Rep Power: 15
Luigi_ is on a distinguished road
Thanks, I had not know about that quantity in Star. I was able to run a report on that quantity, and I am still well above 1E-5. So I am not so much worried about that anymore.

So to get mesh independence in my BL, I can add prism layers while keeping the overall mesh thickness constant to refine my mesh in this area. That seems to make sense since it is like the bulk flow mesh refinement. But I'm still a little confused about whether I also reduce the size of the outermost prism layer thickness (i'm using this as a specification, as opposed to the stretching method). Right now it is below y+ of 1.0, which is the recomendation for low y+ models. But it seems like since I'm using a low y+ wall treatment, it calculates quantities down to the wall, so a more refined mesh in this region would be better. Can anyone confirm this? Is there a danger of having your outermost prism layer cell too thin/too close to the wall? As long as you have y+ less than 1.0 for that cell, is it just a decision on how much refinement you want in that region?

Thanks again!
Luigi_ is offline   Reply With Quote

Old   December 15, 2011, 09:49
Default
  #6
Senior Member
 
Ryne Whitehill
Join Date: Aug 2009
Posts: 312
Rep Power: 19
rwryne is on a distinguished road
Quote:
Originally Posted by kyle View Post
The prism layer thickness should not be set as a percentage of the base size. This should not even be an option, much less the default behavior.
Completely agree with this. I do not understand why they still have it like this.
rwryne is offline   Reply With Quote

Old   December 17, 2011, 15:43
Default
  #7
Member
 
Join Date: May 2010
Posts: 40
Rep Power: 16
Ladnam is on a distinguished road
"Volume change smaller than 1e5 is OK" is not applicable to all cases.
In some cases volume changes even as low as 10 can give completely wrong result.
Ladnam is offline   Reply With Quote

Old   January 15, 2012, 15:40
Default
  #8
Senior Member
 
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,754
Rep Power: 66
LuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura about
Quote:
Originally Posted by Luigi_ View Post
Thanks, I had not know about that quantity in Star. I was able to run a report on that quantity, and I am still well above 1E-5. So I am not so much worried about that anymore.

So to get mesh independence in my BL, I can add prism layers while keeping the overall mesh thickness constant to refine my mesh in this area. That seems to make sense since it is like the bulk flow mesh refinement. But I'm still a little confused about whether I also reduce the size of the outermost prism layer thickness (i'm using this as a specification, as opposed to the stretching method). Right now it is below y+ of 1.0, which is the recomendation for low y+ models. But it seems like since I'm using a low y+ wall treatment, it calculates quantities down to the wall, so a more refined mesh in this region would be better. Can anyone confirm this? Is there a danger of having your outermost prism layer cell too thin/too close to the wall? As long as you have y+ less than 1.0 for that cell, is it just a decision on how much refinement you want in that region?

Thanks again!
Once you have your y+ criterion satisfied, you just need to make sure you have "enough" cells to completely resolve the boundary layer. Normally this means making sure that there is a gradual growth in cell size until you approach the core mesh size. Because the cell size closest to the wall for y+ <1 is already small, usually there is not a problem of the outermost cell being "too small" if the volume change is already gradual.
LuckyTran is offline   Reply With Quote

Reply

Tags
boundary layer


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Turbulent Boundary Layer on a Flat Plate Hoshang Garda FLUENT 1 November 27, 2013 11:24
LES- first grid point in boundary layer, y+ sina Main CFD Forum 0 February 3, 2011 10:26
[snappyHexMesh] Boundary layer generation problems ivan_cozza OpenFOAM Meshing & Mesh Conversion 0 October 6, 2010 14:47
Boundary Layer Question scottneh STAR-CCM+ 3 September 30, 2010 15:21
Errors in Gambit for boundary layer mesh Mike Spears FLUENT 0 June 23, 2005 12:34


All times are GMT -4. The time now is 22:07.